Chap.6 The Impulse-Momentum Principle
• So far, we have studied the flow characteristics (velocity, pressure, etc.) in a fluid. In this chapter, we study the force acting on a structure by fluid in a flow. As for the force acting on a structure in quiescent fluid, we studied it in Chapter 2.
• Newton’s 2nd law (in a vector form):
( )
cc mv
dt a d
m
F = =
∑
where vc = velocity of the center of mass of the system
( ) ( )
12343 42 1
momentum linear time
the in impulse
c
dt
v m d dt F =
∑
• Linear impulse-momentum equation
→ magnitude and direction of resultant forces exerted on fluid by structures (or on structures by fluid)
• Angular impulse-momentum equation
→ line of action of the resultant force
6.1 Linear Impulse-Momentum Equation
For the individual fluid system,
( ) (
vdV)
dt v d
dt m a d
m
F = = = ρ
∑
Summation over the whole flow system:
( )
(
2 1)
1 1 1 2 2
2
CS CS
system system
ext
in out
) (
v )
( v
V V
Q Q
V Q
V
dA n v dA
n v
V d dt v
V d d dt v
F d
−
=
−
=
⋅ +
⋅
=
=
=
∫∫
∫∫
∫∫∫
∑ ∫∫∫
ρ ρ
ρ
ρ ρ
ρ ρ
where
∑
Fext = body force + forces on C.S.(Q all the internal forces b/w individual fluid systems are cancelled out)
(
2 1)
ext Q V V
F = −
∴
∑
ρIn a 2-D flow (x and z),
( ) ( )
( ) ( )
⎪⎭⎪⎬
⎫
−
=
−
=
∑
∑
z z
x x
V V
Q F
V V
Q F
z x
1 2
ext
1 2
ext
ρ ρ
Magnitude and direction of
∑
Fext.But line of action is not known yet.
If the flow enters and leaves at more than one location,
( ) (
out)
inext
∑ ∑
∑
F = QρV − QρV6.2 Pipe Flow Applications
(1) Force acting on pipe bend) cos
( cos
: p1A1 p2A2 F Q V2 V1
x − α − x = ρ α −
Fx = p1A1 − p2A2cosα −Qρ(V2 cosα −V1) ) 0 sin
( sin
: −W − p2A2 α + F =Qρ V2 α −
z z
Fz =W + p2A2sinα +QρV2sinα
(2) Energy loss at abrupt expansion of a passage
Impulse-momentum equation on C.V. ABCD:
) (
)
( 2 1 2 2 2 1
2 2 2
1A p A Q V V AV V V
p
Fx ≈ − = − = −
∑
ρ ρNote: p may be different from p1 in eddy area.
g
V V V p
p1 − 2 = 2( 2 − 1)
∴ γ
Work-energy equation:
g V p
g V p
(EL) 2 2
2 2 2
2 1
1 + −Δ = +
γ γ
g V V
g V V V g
V V
p p
2 )
( (EL) 2
2 2 2 1 1
2 2 2
2 2 1 2
1 − + − = − + −
= Δ
∴ γ
g V V
2 ) ( 1 − 2 2
= : Borda-Carnot head loss
6.3 Open Channel Flow Applications
(1) Force acting on a sluice gate( )
⎟⎟⎠
⎜⎜ ⎞
⎝
⎛ −
=
−
=
−
−
∑
=1 2
1 2 2
2 2
1
ext ( )
2
2 y
q y
q q V
V Q y F
F y x
x γ γ ρ ρ
( )
⎟⎟⎠
⎜⎜ ⎞
⎝
⎛ −
−
−
=
∴
1 2
2 2
2 2
1
1 1
2 y y q y y
Fx γ ρ
⊥
F gate (Q no shear force for ideal fluid) Fx
F =
∴ cosθ →
θ cos
Fx
F =
θ sin F Fz =
No need for impulse-momentum equation in z- direction.
See IP 6.2 (p 197) for horizontal force acting on an overflow structure (same principle).
(2) Energy loss due to hydraulic jump
Impulse-momentum equation:
( )
( )2
2 2 1
2 2 2
1
ext y y q V V
F x = − = −
∑
γ γ ρ ← no structureno external force by structure Continuity: q =V1y1 =V2y2 →
2 2
1
1 ,
y V q
y
V = q =
( )
⎟⎟⎠
⎜⎜ ⎞
⎝
⎛ −
=
−
∴
1 2
2 2
2 2
1
1 1
2g y y q ρ y y
ρ
⎟⎟⎠
⎜⎜ ⎞
⎝
⎛ −
=
−
2 1
2 2
1 2 2
1 1
2
y y
g y q
y
( )( )
2 1
1 2 2 1
2 1 2
2
y y
y y
g y q
y y
y + − = −
2 0
3 1
2
1 2 2
1
2 ⎟⎟⎠ + − =
⎜⎜ ⎞
⎝
⎛
gy q y
y y
y
⎟⎟
⎠
⎞
⎜⎜
⎝
⎛− + +
⎟ =
⎟
⎠
⎞
⎜⎜
⎝
⎛− + +
=
∴
1 2 1 3
1 2
1
2 8
1 2 1
1 1 8
2 1 1
gy V gy
q y
y
(a) 1
1 2 2 1
1 = =
gy
F V → 1
1 2 = y
y ; no hydraulic jump
(b) 1
1 2 2 1
1 = >
gy
F V → 1
1 2 >
y
y ; hydraulic jump occurs
(c) 1
1 2 2 1
1 = <
gy
F V → 1
1 2 <
y
y ; physically impossible Note: = = Froudenumber
gy F V
⎟⎟⎠
⎜⎜ ⎞
⎝
⎛ +
⎟⎟−
⎠
⎜⎜ ⎞
⎝
⎛ +
⎟⎟ =
⎠
⎜⎜ ⎞
⎝
⎛ +
⎟⎟ −
⎠
⎜⎜ ⎞
⎝
⎛ +
=
Δ 2
2 2 2 2
1 2 1
2 2 2
2 1
1 2 2 2 2
) EL
( gy
y q gy
y q g
y V g
y V
Using ( )
2 1 2 1 2
2 g y y y y
q = +
( )
4 0 EL)
(
2 1
3 1 2 − >
=
Δ y y
y
y for energy loss
1
2 y
y >
∴ → 1
1 2 >
y y
(3) Velocity of small gravity waves
not fluid velocity but propagating speed of waves
Under the wave, fluid velocity is unknown except that it is constant over depth for a small gravity wave (or long wave).
For a stationary observer, it is an unsteady problem. For an observer moving with speed a, however, it is a steady problem.
Continuity: ay =V(y + dy) = q
Impulse-momentum: ( )
2 ) (
2
2 2
a V dy q
y
y + = −
− γ ρ
γ
⎟⎠
⎜ ⎞
⎝⎛ +
⎟⎠
⎜ ⎞
⎝
⎛ +
=
∴ y dy
y g dy
a 2
1 1
2
If y >> dy, then a ≈ gy ← a depends only on y.
6.4 Angular Impulse-Momentum Principle
line of action of resultant forces( ∑F = ma)moment→ moment of momentum
= angular momentum
( ) ( ) (
r v dV)
dt v d
m dt r
a d m r F
r× = × = × = × ρ
∑
Summation over the whole flow system:
( ) ∫∫∫ ( )
∑
× = ×sys
ext r v dV
dt F d
r ρ
( ) ( ) ( ) ( ∫∫ )
∫∫
× ⋅ + × ⋅=
in
out CS
CS
dA n v v r dA
n v v
r ρ ρ
( ) ∫∫ ( )
∫∫
× − ×=
in
out CS
CS
dQ v
r dQ
v
r ρ ρ
(
rout Vout)
Q(
rin Vin)
Q × − ×
= ρ ρ
( ) ( ) [
r V out r V in]
Q × − ×
= ρ
( ) ∑ [ ( ) ( ) ]
∑
× = = × − ×∴ r Fext M 0 Qρ r V out r V in
Note: r = xi + y j + zk, V =Vxi +Vy j +Vzk
(
yV zV)
i(
zV xV)
j(
xV yV)
kV V
V
z y x
k j i
V
r z y x z y x
z y x
− +
− +
−
=
=
×
In 2-D problem (x,z),
(
zV xV)
j VV
z x
k j i V
r x z
z x
−
=
=
×
0 0
Similarly, r×F =
(
zFx − xFz)
j( ) [ ( ) ( ) ]
∑
− = − − −∴ zFextx xFextz Qρ z2V2x x2V2z z1V1x x1V1z
where 1=CSin and 2=CSout.
For the resultant force, use Fext ×r , where Fext is known from linear impulse-momentum equation. For other external forces (i.e. body force and pressure forces at 1 and 2), we know the point of action (i.e. x and z).